Cost Effective On Demand Flow Control Shape Memory Alloy Actuators

Award Information
Agency:
National Aeronautics and Space Administration
Branch
n/a
Amount:
$599,862.00
Award Year:
2002
Program:
SBIR
Phase:
Phase II
Contract:
NAS1-02060
Award Id:
57170
Agency Tracking Number:
000749
Solicitation Year:
n/a
Solicitation Topic Code:
n/a
Solicitation Number:
n/a
Small Business Information
Continuum Dynamics, Inc. (Currently CONTINUUM DYNAMICS INC)
34 Lexington Avenue, Ewing, NJ, 08618
Hubzone Owned:
N
Minority Owned:
N
Woman Owned:
N
Duns:
n/a
Principal Investigator:
Alan Bilanin
Senior Associate
(609) 538-0444
alan@cdiprinceton.com
Business Contact:
Barbara Agans
Administrator
(609) 538-0444
alan@cdiprinceton.com
Research Institution:
n/a
Abstract
The development of new, active flow control devices will be critical to meeting the NASA Aerospace Technology Enterprise goals of reducing air travel costs by 25% in 10 years and 50% in 25 years. Continuum Dynamics, Inc. (CDI) proposes the development of a new ¿pop-up¿ vortex generator (PUVG) concept which will eliminate cruise and off-design drag penalties of conventional vortex generators through flush surface stowage and deliver the proven flow control of traditional vortex and micro-vortex generators when deployed. Key in the development of this new flow control device is the application of Shape Memory Alloy (SMA) technologies developed at CDI which allow: device stowage conforming to the application mold line; minimum power requirements through self-locking actuation; low weight and simplicity through elimination of bulky mechanical actuation; the potential for selective deployment optimization based on vehicle operating conditions; and the potential for retrofit on existing aircraft systems. The proposed Phase I effort will carry out the conceptual design, fabrication and experimental studies demonstrating ¿proof of concept,¿ which can then be carried to Phase II/III product development. PUVGs offer the building blocks for a distributed flow control system with the potential to optimize aircraft performance in critical flight conditions.

* information listed above is at the time of submission.

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